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The propulsive power of the rocket is (where v1 = Jet velocity and v2 = Aircraft velocity)

The propulsive power of the rocket is (where v1 = Jet velocity and v2 = Aircraft velocity) Correct Answer $$\frac{{{\text{v}}_1^2 - {\text{v}}_2^2}}{{2{\text{g}}}}$$

The propulsive power of the rocket is $$\frac{{{\text{v}}_1^2 - {\text{v}}_2^2}}{{2{\text{g}}}}$$
Where ,
v1 = Jet velocity
v2 = Aircraft velocity

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